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Pratt & Whitney Engines
F100-PW-229 TURBOFAN ENGINE

p&weng04.jpg (45414 bytes)

Aircraft used on (click here)

 

Engine Characteristic
Maximum Thrust (Full Augmentation) 29,100 lb (129.4 kN)
Intermediate Thrust (Nonaugmented) 17,800 Ib (79.2 kN)
Weight (Specification Maximum) 3,740 lb (1,681 kg)
Length 191 in. (4.85 m)
Inlet Diameter 34.8 in. (0.88 m)
Maximum Diameter 46.5 in. (1. 18 in)
Bypass Ratio 0.36
Overall Pressure Ratio 32 to 1

 

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Updated: February 23, 1999